2014 Aluminum T6
Verifiedmetal· T651
2014-T6 is a copper-alloyed aluminum alloy in the 2xxx series, solution heat-treated and artificially aged to peak strength, offering high yield strength (typical 60 ksi) and ultimate tensile strength (typical 70 ksi) with moderate ductility for aerospace structural applications requiring fatigue resistance. Primary applications include aircraft fuselage and wing components, forgings, and structural details where strength-to-weight ratio and bearing load capability are critical, with continuous service capability to approximately 250°F.
aerospacestructural
Compliance & Regulations
?Conflict Free?FDA?RoHS?REACH?TSCA?Prop 65
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Specification
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Ultimate Bearing Strength(Fbru) | — | Pa | 40 entriesClick to expand | ||
Bearing Yield Strength(Fbry) | — | Pa | 47 entriesClick to expand | ||
Bending Rupture Ratio (Fb/Ftu) vs D/t(Fb/Ftu) | Curve (10 pts) | - | — | — | |
Compressive Modulus(Ec) | — | Pa | 22°C · Bar/Extrusion/Rod | — | |
Compressive Tangent Modulus vs Stress(Etn(σ)) | — | Pa | 18 entriesClick to expand | ||
Compressive Yield Strength(Fcy) | — | Pa | 61 entriesClick to expand | ||
Elongation at Break(εf) | — | - | 60 entriesClick to expand | ||
Poisson's Ratio(ν) | — | - | 22°C | — | |
Shear Modulus(G) | — | Pa | 22°C · Bar/Extrusion/Rod | — | |
Ultimate Shear Strength(Fsu) | — | Pa | 24 entriesClick to expand | ||
S–N Curve (Wöhler)(S–N) | — | Pa | 20 entriesClick to expand | ||
Stress–Strain Curve(σ–ε)2 entries | Curve (10 pts) | Pa | 21°C · L | — | |
| ↳ | Curve (9 pts) | Pa | 21°C · LT | — | |
Stress–Strain Curve (buckling region, ≤ 2% strain)(σ–ε (low-strain)) | — | Pa | 25 entriesClick to expand | ||
Torsional Modulus of Rupture vs D/t(Fst(D/t)) | — | Pa | 16 entriesClick to expand | ||
Ultimate Tensile Strength(σUTS) | — | Pa | 74 entriesClick to expand | ||
Yield Strength (0.2% offset)(σy) | — | Pa | 78 entriesClick to expand | ||
Young's Modulus(E) | — | Pa | 22°C · Bar/Extrusion/Rod | — | |
N entriesMultiple entries per property — large groups are collapsed; click a summary row to expand. Use filters above to narrow by form / heat treatment / basis.
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
CTE vs Temperature(α(T)) | Curve (9 pts) | 1/K | — | — | |
Specific Heat vs Temperature(Cp(T)) | Curve (4 pts) | J/(kg·K) | — | — | |
Thermal Conductivity vs Temperature(k(T)) | Curve (8 pts) | W/(m·K) | — | — |
Verified Unverified Low confidence (<80%) Link to source
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | — | kg/m³ | 22°C | — |
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source
Regulatory Screening
Environmental
Safety & Biocompatibility
Quality & Standards
RoHS, REACH, and Prop 65 statuses are validated against official substance lists (ECHA SVHC Candidate List, OEHHA Prop 65, RoHS Annex II). Other regulations are estimated from composition and material classification. All screening is a starting point for due diligence — always verify with your supplier before making compliance decisions.